Skyleader 600

metal two-seat

Max speed
265 km/h

Range
1600 km

Category
UL/LSA

Capacity
2

The SKYLEADER 600 is an all metal two-seat, low wing constructed aircraft with a trapezoidal wing. The aircraft has a tricycle towed fixed landing gear with wheel pants and a steerable nose wheel, either retractable gear option. The aircraft are designated mainly for recreational flying, pilot training and special operations.

Aircraft can be customized based on your requirements. You will be impressed by the high safety standards, impressive flight characteristics and timeless design which is the result of real ASTM certified aeronautical production. Easy repairs & maintenance guarantees the low operational costs.

Simply: Our aircraft provide safety, prestige and emotion to customers around the world.

Photogallery

TECHNICAL DATA

SPEEDS KILOMETERS KNOTS MILES
Never exceed speed (VNE) 265 km/h 143 knots 165 mph
Cruise speed @ 75% power (VC) 220 km/h 122 knots 137 mph
Maneuvering speed (VA) 145 km/h 78 knots 90 mph
Min. speed without flaps (VS1) 72 km/h 39 knots 44 mph
Min. speed with flaps (VS0) 61 km/h 33 knots 37 mph
WEIGHT
Weight UL / LSA up to 600 kg / 1320 lbs.
Basic empty weight 320 kg / 705 lbs.
ENGINE & PROPELLER
Engine type Rotax® 912 UL, ULS ; 914 UL ; 912iS fuel injection
Maximum power (80HP) – 115HP turbocharged
Propeller 2 or 3 – blade on the ground or in flight adjustable
FUEL CAPACITY & ENDURANCE
Fuel capacity 120 L / 31.8 US gal / 198 lbs / 90 kg
Endurance 8.5 + 0.5 h
Range 1600 km / 860 nm / 1000 miles
TAKE-OFF & LANDING
Take-off distance 250 m / 820 ft
Take-off run 90 – 100 m / 300 – 330 ft
Landing distance 200 m / 660 ft
Landing run 100 m / 330 ft
DIMENSIONS
Wing span 9.9 m / 32 ft 4.5 in
Overall length 7.1 m / 23 ft 3.5 in
Overall height 2.46 m / 8 ft
Wing area 11.85 m2 / 127.5 sq. ft
Aspect ration 7.78
Cabin width 1.28 m / 4 ft 2 in

*Values depending on the aircraft configuration